Effect of rib turbulators in the first pass on heat transfer distributions in a two-pass channel connected by two rows of holes

Proceedings of the ASME Turbo Expo

Volumn 3, Issue , 2001, Pages

  Ekkad, Srinath V ^a   Kontrovitz, David ^a   Nasir, Hasan ^a   Pamula, Gautam ^a   Acharya, Sumanta ^a  

^a LOUISIANA STATE UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COOLANTS; FACINGS; REYNOLDS NUMBER; SERPENTINE; TURBOMACHINERY;

COOLANT PASSAGES; ENHANCED HEAT TRANSFER; GAS TURBINE BLADES; HEAT TRANSFER DISTRIBUTIONS; HEAT TRANSFER ENHANCEMENT; INTERNAL CHANNEL; SERPENTINE CHANNEL; TWO-PASS CHANNEL;

HEAT TRANSFER COEFFICIENTS;

EID: 82055208723     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/2001-GT-0184     Document Type: Conference Paper

References (15)

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